Torque vs Motor Input Current for Coolant Pump Motor, P/N 52-83700-403, S/N 123-111.

Abstract

The test request was initiated to determine the electrical stall characteristics of either the motors used in the Coolant Pump Assembly. The coolant pump motor is a 3-phase, 60 cycle, 12 v rms unit. It is installed in coolant pump assemblies to drive the gears of the pump cartridge which establishes the flow of coolant fluid in the spacecraft. This system was utilized in the Gemini 'A' spacecraft, and it is proposed for use in the Gemini 'B' and Airlock programs. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 08, 1967
Accession Number
AD0856652

Entities

People

  • Craig A. Meier

Tags

DTIC Thesaurus Topics

  • Assembly
  • Coolant Pumps
  • Pumps
  • Spacecraft

Readers

  • Aerospace Test and Evaluation
  • Combustion and Flow Dynamics.
  • Software Engineering

Technology Areas

  • Space
  • Space - Hall-Effect Thruster